TWI646759B - Charge and discharge pump circuit and control method thereof - Google Patents
Charge and discharge pump circuit and control method thereof Download PDFInfo
- Publication number
- TWI646759B TWI646759B TW106126147A TW106126147A TWI646759B TW I646759 B TWI646759 B TW I646759B TW 106126147 A TW106126147 A TW 106126147A TW 106126147 A TW106126147 A TW 106126147A TW I646759 B TWI646759 B TW I646759B
- Authority
- TW
- Taiwan
- Prior art keywords
- period
- timing control
- charge
- flying capacitor
- discharging
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 29
- 239000003990 capacitor Substances 0.000 claims abstract description 143
- 238000007599 discharging Methods 0.000 claims abstract description 100
- 230000003213 activating effect Effects 0.000 claims 1
- 230000001360 synchronised effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 14
- 101000772173 Homo sapiens Tubby-related protein 1 Proteins 0.000 description 3
- 101000677914 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) 40S ribosomal protein S5 Proteins 0.000 description 3
- 102100029293 Tubby-related protein 1 Human genes 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G3/00—Control arrangements or circuits, of interest only in connection with visual indicators other than cathode-ray tubes
- G09G3/20—Control arrangements or circuits, of interest only in connection with visual indicators other than cathode-ray tubes for presentation of an assembly of a number of characters, e.g. a page, by composing the assembly by combination of individual elements arranged in a matrix no fixed position being assigned to or needed to be assigned to the individual characters or partial characters
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09G—ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION
- G09G2320/00—Control of display operating conditions
- G09G2320/02—Improving the quality of display appearance
- G09G2320/0209—Crosstalk reduction, i.e. to reduce direct or indirect influences of signals directed to a certain pixel of the displayed image on other pixels of said image, inclusive of influences affecting pixels in different frames or fields or sub-images which constitute a same image, e.g. left and right images of a stereoscopic display
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- General Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- Dc-Dc Converters (AREA)
Abstract
一種充放電幫浦電路及其控制方法。充放電幫浦電路包括一第一飛行電容、一第二飛行電容及一時序控制器。該第一飛行電容與該第二飛行電容並聯。該時序控制器電性連接於並聯之該第一飛行電容及該第二飛行電容。該時序控制器係以一第一時序控制訊號控制該第一飛行電容,並以一第二時序控制訊號控制該第二飛行電容,該第一時序控制訊號不同於該第二時序控制訊號。 A charge and discharge pump circuit and a control method thereof. The charging and discharging pump circuit includes a first flying capacitor, a second flying capacitor, and a timing controller. The first flying capacitor is connected in parallel with the second flying capacitor. The timing controller is electrically connected to the first flying capacitor and the second flying capacitor in parallel. The timing controller controls the first flying capacitor with a first timing control signal, and controls the second flying capacitor with a second timing control signal. The first timing control signal is different from the second timing control signal. .
Description
本發明是有關於一種電子電路及其控制方法,且特別是有關於一種充放電幫浦(charge-discharge pump)電路及其控制方法。 The invention relates to an electronic circuit and a control method thereof, and in particular to a charge-discharge pump circuit and a control method thereof.
隨著顯示技術的進步,各式顯示面板不斷推陳出新。在顯示面板中,需要提供一負類比電壓(negative AVDD)以進行驅動。 With the development of display technology, various display panels are constantly being introduced. In the display panel, a negative analog voltage (negative AVDD) needs to be provided for driving.
一般而言,負類比電壓可以透過兩種組合電路來實現,第一種組合電路是一升壓電路(boost circuit)與一升壓-降壓轉換電路(buck-boost circuit)之組合,第二種組合電路是升壓電路與充放電幫浦電路(charge-discharge pump circuit)之組合。 Generally speaking, the negative analog voltage can be realized by two combination circuits. The first combination circuit is a combination of a boost circuit and a buck-boost circuit. The second This combination circuit is a combination of a boost circuit and a charge-discharge pump circuit.
由於充放電幫浦電路的成本較低,因此第二種組合電路較為廣泛使用。然而,充放電幫浦電路經常會造成較大的 漣波(ripple),進而在重負載的顯示面板或大尺寸且高解析度之面板容易形成干擾(crosstalk)現象,嚴重影響畫面品質。 Because the cost of the charge and discharge pump circuit is low, the second combination circuit is more widely used. However, charge and discharge pump circuits often cause larger Ripples, in turn, are more likely to form crosstalk phenomena in heavy-load display panels or large-sized and high-resolution panels, which seriously affects picture quality.
本發明係有關於一種充放電幫浦(charge-discharge pump)電路及其控制方法,其利用多個飛行電容交錯地進行充放電動作,使得整體充電的間隔縮短,而能夠減少負類比電壓的漣波(ripple),進而避免產生干擾(crosstalk)現象,以維持良好畫面品質。 The invention relates to a charge-discharge pump circuit and a control method thereof, which use a plurality of flying capacitors to alternately perform a charge-discharge operation, so that the overall charging interval is shortened, and the ripple of negative analog voltage can be reduced. Ripple, thereby avoiding crosstalk, so as to maintain good picture quality.
根據本發明之第一方面,提出一種充放電幫浦(charge-discharge pump)電路。充放電幫浦電路包括一第一飛行電容(flying capacitor)、一第二飛行電容及一時序控制器。該第一飛行電容與該第二飛行電容並聯。該時序控制器電性連接於並聯之該第一飛行電容及該第二飛行電容。該時序控制器係以一第一時序控制訊號控制該第一飛行電容,並以一第二時序控制訊號控制該第二飛行電容,該第一時序控制訊號不同於該第二時序控制訊號。 According to a first aspect of the present invention, a charge-discharge pump circuit is provided. The charging and discharging pump circuit includes a first flying capacitor, a second flying capacitor, and a timing controller. The first flying capacitor is connected in parallel with the second flying capacitor. The timing controller is electrically connected to the first flying capacitor and the second flying capacitor in parallel. The timing controller controls the first flying capacitor with a first timing control signal, and controls the second flying capacitor with a second timing control signal. The first timing control signal is different from the second timing control signal. .
根據本發明之一第二方面,提出一種充放電幫浦(charge-discharge pump)電路之控制方法。該充電幫浦電路包括一第一飛行電容(flying capacitor)及一第二飛行電容,該第一飛行電容與該第二飛行電容並聯。該控制方法包括以下步驟:以一第一時序控制訊號控制該第一飛行電容。以一第二時序 控制訊號控制該第二飛行電容,該第一時序控制訊號不同於該第二時序控制訊號。 According to a second aspect of the present invention, a method for controlling a charge-discharge pump circuit is proposed. The charging pump circuit includes a first flying capacitor and a second flying capacitor, and the first flying capacitor is connected in parallel with the second flying capacitor. The control method includes the following steps: controlling the first flying capacitor with a first timing control signal. At a second timing The control signal controls the second flying capacitor, and the first timing control signal is different from the second timing control signal.
為了對本發明之上述及其他方面有更佳的瞭解,下文特舉實施例,並配合所附圖式詳細說明如下: In order to have a better understanding of the above and other aspects of the present invention, the following specific examples are described in detail below in conjunction with the accompanying drawings:
100、400‧‧‧充放電幫浦電路 100, 400‧‧‧charge and discharge pump circuit
110‧‧‧第一飛行電容 110‧‧‧First flying capacitor
120‧‧‧第二飛行電容 120‧‧‧Second flying capacitor
150‧‧‧時序控制器 150‧‧‧sequence controller
151‧‧‧第一控制器 151‧‧‧The first controller
152‧‧‧第二控制器 152‧‧‧Second controller
161‧‧‧第一開關 161‧‧‧The first switch
162‧‧‧第二開關 162‧‧‧Second switch
163‧‧‧第三開關 163‧‧‧Third switch
164‧‧‧第四開關 164‧‧‧Fourth switch
430‧‧‧第三飛行電容 430‧‧‧Third flying capacitor
453‧‧‧第三控制器 453‧‧‧Third controller
465‧‧‧第五開關 465‧‧‧Fifth switch
466‧‧‧第六開關 466‧‧‧ sixth switch
IN‧‧‧輸入端 IN‧‧‧Input
A、B‧‧‧點 A, B‧‧‧ points
C41、C42、C51、C52、C53、C101、C102、C103、C141、C142、C143、C144‧‧‧曲線 C41, C42, C51, C52, C53, C101, C102, C103, C141, C142, C143, C144‧‧‧ curves
CY1、CY2、CY4‧‧‧週期 CY1, CY2, CY4 ‧‧‧ cycles
OUT‧‧‧輸出端 OUT‧‧‧output
RP4、RP5、RP10、RP14‧‧‧突波 RP4, RP5, RP10, RP14‧‧‧ surge
S210、S220、S610、S620、S630、S640、S650‧‧‧步驟 S210, S220, S610, S620, S630, S640, S650‧‧‧ steps
SR‧‧‧訊號輸入端 SR‧‧‧Signal input
sw‧‧‧切換訊號 sw‧‧‧ switch signal
T1、T2‧‧‧期間 During T1, T2‧‧‧
T21、T31、T41‧‧‧第一充電期間 T21, T31, T41‧‧‧First charging period
T22、T32、T42‧‧‧第一放電期間 T22, T32, T42‧‧‧First discharge period
T23、T33、T43‧‧‧第二充電期間 T23, T33, T43‧‧‧Second charging period
T24、T34、T44‧‧‧第二放電期間 T24, T34, T44‧‧‧Second discharge period
T45‧‧‧第三充電期間 T45‧‧‧The third charging period
T46‧‧‧第三放電期間 T46‧‧‧The third discharge period
ts11、ts21、ts31、ts41‧‧‧第一時序控制訊號 ts11, ts21, ts31, ts41 ‧‧‧ the first timing control signal
ts12、ts22、ts32、ts42‧‧‧第二時序控制訊號 ts12, ts22, ts32, ts42‧‧‧Second timing control signal
ts43‧‧‧第三時序控制訊號 ts43‧‧‧third timing control signal
第1圖繪示根據本發明之一實施例之一充放電幫浦電路(charge-discharge pump circuit)之示意圖。 FIG. 1 is a schematic diagram of a charge-discharge pump circuit according to an embodiment of the present invention.
第2圖繪示根據本發明之一實施例之充放電幫浦電路之控制方法的流程圖。 FIG. 2 is a flowchart of a control method of a charge-discharge pump circuit according to an embodiment of the present invention.
第3圖繪示根據本發明一實施例之一第一時序控制訊號及一第二時序控制訊號之示意圖。 FIG. 3 is a schematic diagram of a first timing control signal and a second timing control signal according to an embodiment of the present invention.
第4圖繪示僅透過第一時序控制訊號進行充放電操作之第一飛行電容與輸出端之充放電曲線。 FIG. 4 shows the charging and discharging curves of the first flying capacitor and the output terminal for charging and discharging operation only through the first timing control signal.
第5圖繪示同時透過第一時序控制訊號及第二時序控制訊號進行充放電操作之第一飛行電容、第二飛行電容與輸出端之充放電曲線。 FIG. 5 shows the charging and discharging curves of the first flying capacitor, the second flying capacitor, and the output terminal through the first timing control signal and the second timing control signal for charging and discharging at the same time.
第6圖繪示根據本發明另一實施例之充放電幫浦電路之控制方法的流程圖。 FIG. 6 is a flowchart of a control method of a charge-discharge pump circuit according to another embodiment of the present invention.
第7圖繪示第一模式之操作示意圖。 FIG. 7 illustrates the operation of the first mode.
第8圖繪示第二模式之操作示意圖。 FIG. 8 illustrates the operation of the second mode.
第9圖繪示根據本發明另一實施例之一第一時序控制訊號及一第二時序控制訊號之示意圖。 FIG. 9 is a schematic diagram of a first timing control signal and a second timing control signal according to another embodiment of the present invention.
第10圖繪示同時透過第一時序控制訊號及第二時序控制訊號進行充放電操作之第一飛行電容、第二飛行電容與輸出端之充放電曲線。 FIG. 10 shows the charging and discharging curves of the first flying capacitor, the second flying capacitor, and the output terminal, which are charged and discharged simultaneously through the first timing control signal and the second timing control signal.
第11圖繪示根據本發明另一實施例之一第一時序控制訊號及一第二時序控制訊號之示意圖。 FIG. 11 is a schematic diagram of a first timing control signal and a second timing control signal according to another embodiment of the present invention.
第12圖繪示根據本發明另一實施例之充放電幫浦電路之示意圖。 FIG. 12 is a schematic diagram of a charge-discharge pump circuit according to another embodiment of the present invention.
第13圖繪示根據本發明一實施例之第一時序控制訊號、第二時序控制訊號及第三時序控制訊號之示意圖。 FIG. 13 is a schematic diagram of a first timing control signal, a second timing control signal, and a third timing control signal according to an embodiment of the present invention.
第14圖繪示同時透過第一時序控制訊號、第二時序控制訊號及第三時序控制訊號進行充放電操作之第一飛行電容、第二飛行電容、第三飛行電容與輸出端之充放電曲線。 Figure 14 shows the first flying capacitor, the second flying capacitor, the third flying capacitor, and the output terminal charging and discharging at the same time through the first timing control signal, the second timing control signal, and the third timing control signal. curve.
請參照第1圖,其繪示根據本發明之一實施例之一充放電幫浦電路(charge-discharge pump circuit)100之示意圖。充放電幫浦電路100包括一第一飛行電容110、一第二飛行電容120、一時序控制器150、一第一控制器151、一第二控制器152、一第一開關161、一第二開關162、一第三開關163及一第四開關164。第一飛行電容110與第二飛行電容120並聯。時序控制器150電性連接於並聯之第一飛行電容110及第二飛行電容 120。第一飛行電容110及第二飛行電容120耦接於同一輸入端IN,且第一飛行電容110及第二飛行電容120耦接於同一輸出端OUT,以提供負類比電壓(negative AVDD)。 Please refer to FIG. 1, which illustrates a schematic diagram of a charge-discharge pump circuit 100 according to an embodiment of the present invention. The charging and discharging pump circuit 100 includes a first flying capacitor 110, a second flying capacitor 120, a timing controller 150, a first controller 151, a second controller 152, a first switch 161, and a second The switch 162, a third switch 163, and a fourth switch 164. The first flying capacitor 110 is connected in parallel with the second flying capacitor 120. The timing controller 150 is electrically connected to the first flying capacitor 110 and the second flying capacitor in parallel. 120. The first flying capacitor 110 and the second flying capacitor 120 are coupled to the same input terminal IN, and the first flying capacitor 110 and the second flying capacitor 120 are coupled to the same output terminal OUT to provide a negative AVDD.
第一飛行電容110、第一開關161及第二開關162組成第一級電路,第二飛行電容120、第三開關163及第四開關164組成第二級電路。第一飛行電容110及第二飛行電容120各自可進行充放電的動作。在本實施例中,第一飛行電容110及第二飛行電容120可以交錯地進行充放電動作,使得整體充電的間隔縮短,而能夠減少負類比電壓的漣波(ripple),進而避免產生干擾(crosstalk)現象,以維持良好畫面品質。 The first flying capacitor 110, the first switch 161, and the second switch 162 constitute a first-stage circuit, and the second flying capacitor 120, the third switch 163, and the fourth switch 164 constitute a second-stage circuit. Each of the first flying capacitor 110 and the second flying capacitor 120 can perform charging and discharging operations. In this embodiment, the first flying capacitor 110 and the second flying capacitor 120 can alternately perform charging and discharging operations, so that the overall charging interval is shortened, and the ripple of the negative analog voltage can be reduced, thereby avoiding interference ( crosstalk) phenomenon to maintain good picture quality.
請參照第2圖及第3圖,第2圖繪示根據本發明之一實施例之充放電幫浦電路100之控制方法的流程圖,第3圖繪示根據本發明一實施例之一第一時序控制訊號ts11及一第二時序控制訊號ts12之示意圖。在步驟S210中,時序控制器150以第一時序控制訊號ts11控制第一飛行電容110。第一控制器151接收到第一時序控制訊號ts11後,依據第一時序控制訊號ts11同步控制第一開關161及第二開關162。舉例來說,在第一時序控制訊號ts11於期間T1為高位準時,第一控制器151同步將第一開關161及第二開關162切往點B,以使第一飛行電容110對輸出端OUT進行充電。在第一時序控制訊號ts11於期間T2為低位準時,第一控制器151同步將第一開關161及第二開關162切往點A,以使輸出端OUT放電。 Please refer to FIG. 2 and FIG. 3. FIG. 2 shows a flowchart of a control method of a charge-discharge pump circuit 100 according to an embodiment of the present invention, and FIG. 3 shows a first embodiment of the first embodiment of the present invention. A schematic diagram of a timing control signal ts11 and a second timing control signal ts12. In step S210, the timing controller 150 controls the first flying capacitor 110 with a first timing control signal ts11. After receiving the first timing control signal ts11, the first controller 151 synchronously controls the first switch 161 and the second switch 162 according to the first timing control signal ts11. For example, when the first timing control signal ts11 is at a high level during the period T1, the first controller 151 synchronously cuts the first switch 161 and the second switch 162 to point B, so that the first flying capacitor 110 pairs the output terminal. OUT for charging. When the first timing control signal ts11 is at a low level during the period T2, the first controller 151 switches the first switch 161 and the second switch 162 to point A synchronously to discharge the output terminal OUT.
在步驟S220中,時序控制器150以第二時序控制訊號ts12控制第二飛行電容120。第二控制器152接收到第二時序控制訊號ts12後,依據第二時序控制訊號ts12同步控制第三開關163及第四開關164。舉例來說,在第二時序控制訊號ts12於期間T2為高位準時,第二控制器152同步將第三開關163及第四開關164切往點B,以使第二飛行電容120對輸出端OUT進行充電。在第二時序控制訊號ts12於期間T1為低位準時,第二控制器152同步將第三開關163及第四開關164切往點A,以使輸出端OUT放電。 In step S220, the timing controller 150 controls the second flying capacitor 120 with a second timing control signal ts12. After receiving the second timing control signal ts12, the second controller 152 synchronously controls the third switch 163 and the fourth switch 164 according to the second timing control signal ts12. For example, when the second timing control signal ts12 is at a high level during the period T2, the second controller 152 switches the third switch 163 and the fourth switch 164 to point B synchronously, so that the second flying capacitor 120 pairs the output terminal OUT Charge it. When the second timing control signal ts12 is at a low level during the period T1, the second controller 152 switches the third switch 163 and the fourth switch 164 to point A synchronously to discharge the output terminal OUT.
上述之步驟S210與步驟S220係可同時執行。步驟S210之第一時序控制訊號ts11不同於步驟S220之第二時序控制訊號ts12。如第3圖所示,第一時序控制訊號ts11相反於第二時序控制訊號ts12。也就是說,在第一飛行電容110於期間T1對輸出端OUT進行充電時,第二飛行電容120於期間T1對輸出端OUT進行放電;在第一飛行電容110於期間T2對輸出端OUT進行放電時,第二飛行電容120於期間T2對輸出端OUT進行充電。 The above steps S210 and S220 can be performed simultaneously. The first timing control signal ts11 in step S210 is different from the second timing control signal ts12 in step S220. As shown in FIG. 3, the first timing control signal ts11 is opposite to the second timing control signal ts12. That is, when the first flying capacitor 110 charges the output terminal OUT during the period T1, the second flying capacitor 120 discharges the output terminal OUT during the period T1; the first flying capacitor 110 charges the output terminal OUT during the period T2. During discharge, the second flying capacitor 120 charges the output terminal OUT during a period T2.
請參照第4圖,其繪示僅透過第一時序控制訊號ts11進行充放電操作之第一飛行電容110與輸出端OUT之充放電曲線。曲線C41為第一飛行電容110之充放電曲線,曲線C42為輸出端OUT之充放電曲線。如曲線C41所示,第一飛行電容110在一個週期CY1進行一次充電動作。如曲線C42所示,輸出端OUT在 一個周期CY1內會形成一個突波RP4,此一突波RP4過大時,則會使類比電壓(AVDD)產生明顯的漣波(ripple)。 Please refer to FIG. 4, which shows the charging and discharging curves of the first flying capacitor 110 and the output terminal OUT that are only charged and discharged through the first timing control signal ts11. Curve C41 is the charge and discharge curve of the first flying capacitor 110, and curve C42 is the charge and discharge curve of the output terminal OUT. As shown by curve C41, the first flying capacitor 110 performs a charging operation in one cycle CY1. As shown by curve C42, the output OUT is at A surge RP4 will be formed in a cycle CY1. When this surge RP4 is too large, the analog voltage (AVDD) will have a significant ripple.
請參照第5圖,其繪示同時透過第一時序控制訊號ts11及第二時序控制訊號ts12進行充放電操作之第一飛行電容110、第二飛行電容120與輸出端OUT之充放電曲線。曲線C51為第一飛行電容110之充放電曲線,曲線C52為第二飛行電容120之充放電曲線,曲線C53為輸出端OUT之充放電曲線。如曲線C51所示,第一飛行電容110在一個週期CY1進行一次充電動作。如曲線C51所示,第二飛行電容120在同一周期CY1也進行一次充電動作。因此,如曲線C53所示,輸出端OUT在一個周期CY1內會形成兩個較小的突波RP5,縮小的突波RP5,可以使類比電壓(AVDD)的漣波變得不明顯。 Please refer to FIG. 5, which shows the charging and discharging curves of the first flying capacitor 110, the second flying capacitor 120, and the output terminal OUT, which are charged and discharged simultaneously through the first timing control signal ts11 and the second timing control signal ts12. Curve C51 is the charge and discharge curve of the first flying capacitor 110, curve C52 is the charge and discharge curve of the second flying capacitor 120, and curve C53 is the charge and discharge curve of the output terminal OUT. As shown by the curve C51, the first flying capacitor 110 performs a charging operation in one cycle CY1. As shown by curve C51, the second flying capacitor 120 also performs a charging operation in the same cycle CY1. Therefore, as shown by the curve C53, the output terminal OUT will form two smaller surges RP5 in one cycle CY1, and the reduced surges RP5 may make the ripple of the analog voltage (AVDD) inconspicuous.
透過上述實施例,充放電幫浦電路100可以透過第一飛行電容110及第二飛行電容120交錯地進行充放電動作,使得整體充電的間隔縮短,而能夠減少負類比電壓的漣波(ripple),進而避免產生干擾(crosstalk)現象,以維持良好畫面品質。 Through the above embodiment, the charge and discharge pump circuit 100 can alternately charge and discharge through the first flying capacitor 110 and the second flying capacitor 120, so that the overall charging interval is shortened, and the ripple of the negative analog voltage can be reduced. , Thereby avoiding crosstalk, so as to maintain good picture quality.
上述實施例對於重負載的顯示面板或大尺寸且高解析度之面板可以有效改善干擾(crosstalk)現象。在採用輕負載、小尺寸或低解析度之面板時,則可透過切換的方式僅使用第一時序控制訊號ts11。 The above embodiments can effectively improve the crosstalk phenomenon for a heavy-duty display panel or a large-sized and high-resolution panel. When a light-load, small-size or low-resolution panel is used, only the first timing control signal ts11 can be used by switching.
請參照第1圖及第6圖,第6圖繪示根據本發明另一實施例之充放電幫浦電路100之控制方法的流程圖。在步驟S610中,充放電幫浦電路100透過一訊號輸入端SR接收一切換訊號sw。在步驟S620中,時序控制器150依據切換訊號sw切換充放電幫浦電路100於一第一模式及一第二模式之間。 Please refer to FIG. 1 and FIG. 6. FIG. 6 shows a flowchart of a control method of the charge-discharge pump circuit 100 according to another embodiment of the present invention. In step S610, the charge and discharge pump circuit 100 receives a switching signal sw through a signal input terminal SR. In step S620, the timing controller 150 switches the charge / discharge pump circuit 100 between a first mode and a second mode according to the switching signal sw.
請參照第7圖,其繪示第一模式之操作示意圖。充放電幫浦電路100於第一模式時,流程進入步驟S630及步驟S640,時序控制器150啟動第一時序控制訊號ts11及第二時序控制訊號ts12,以依據第一時序控制訊號ts11及第二時序控制訊號ts12分別控制第一飛行電容110及第二飛行電容120。 Please refer to FIG. 7, which shows the operation diagram of the first mode. When the charge and discharge pump circuit 100 is in the first mode, the flow proceeds to step S630 and step S640. The timing controller 150 activates the first timing control signal ts11 and the second timing control signal ts12 to control the signal ts11 and The second timing control signal ts12 controls the first flying capacitor 110 and the second flying capacitor 120, respectively.
請參照第8圖,其繪示第二模式之操作示意圖。充放電幫浦電路100於第二模式時,流程進入步驟S650,時序控制器150僅啟動第一時序控制訊號ts11,以依據第一時序控制訊號ts11控制第一飛行電容110。 Please refer to FIG. 8, which shows the operation diagram of the second mode. When the charge and discharge pump circuit 100 is in the second mode, the flow proceeds to step S650, and the timing controller 150 only activates the first timing control signal ts11 to control the first flying capacitor 110 according to the first timing control signal ts11.
如此一來,充放電幫浦電路100能夠依據顯示面板的特性切換於第一模式及第二模式之間,以廣泛地適用於各種類型的顯示面板。 In this way, the charge and discharge pump circuit 100 can be switched between the first mode and the second mode according to the characteristics of the display panel, so as to be widely applicable to various types of display panels.
請參照第9圖,其繪示根據本發明另一實施例之一第一時序控制訊號ts21及一第二時序控制訊號ts22之示意圖。在此實施例中,第一時序控制訊號ts21之一第一充電期間T21大於一第一放電期間T22,第二時序控制訊號ts22之一第二充電期間T23大於一第二放電期間T24。 Please refer to FIG. 9, which illustrates a schematic diagram of a first timing control signal ts21 and a second timing control signal ts22 according to another embodiment of the present invention. In this embodiment, a first charging period T21 of one of the first timing control signals ts21 is greater than a first discharging period T22, and a second charging period T23 of one of the second timing control signals ts22 is greater than a second discharging period T24.
如第9圖所示,第一充電期間T21與第一放電期間T22之比率為2,第二充電期間T23與第二放電期間T24之比率為2。第一充電期間T21涵蓋第二放電期間T24,第二充電期間T23涵蓋第一放電期間T22。此外,第一充電期間T21與第二充電期間T23等長,第一放電期間T22與第二放電期間T24等長。 As shown in FIG. 9, the ratio of the first charging period T21 to the first discharging period T22 is two, and the ratio of the second charging period T23 to the second discharging period T24 is two. The first charging period T21 covers a second discharging period T24, and the second charging period T23 covers a first discharging period T22. The first charging period T21 is the same length as the second charging period T23, and the first discharging period T22 is the same length as the second discharging period T24.
請參照第10圖,其繪示同時透過第一時序控制訊號ts21及第二時序控制訊號ts22進行充放電操作之第一飛行電容110、第二飛行電容120與輸出端OUT之充放電曲線。曲線C101為第一飛行電容110之充放電曲線,曲線C102為第二飛行電容120之充放電曲線,曲線C103為輸出端OUT之充放電曲線。如曲線C101所示,第一飛行電容110在一個週期CY2進行一次充電動作。如曲線C102所示,第二飛行電容120在同一周期CY2也進行一次充電動作。 Please refer to FIG. 10, which shows the charging and discharging curves of the first flying capacitor 110, the second flying capacitor 120, and the output terminal OUT, which are simultaneously charged and discharged through the first timing control signal ts21 and the second timing control signal ts22. Curve C101 is the charge and discharge curve of the first flying capacitor 110, curve C102 is the charge and discharge curve of the second flying capacitor 120, and curve C103 is the charge and discharge curve of the output terminal OUT. As shown by the curve C101, the first flying capacitor 110 performs a charging operation in one cycle CY2. As shown by curve C102, the second flying capacitor 120 also performs a charging operation in the same cycle CY2.
第一飛行電容110及第二飛行電容120之開始充電時間並不相同。因此,如曲線C103所示,輸出端OUT在一個周期CY2內會形成三個較小的突波RP10,縮小的突波RP10可以使類比電壓(AVDD)的漣波變得不明顯。 The initial charging time of the first flying capacitor 110 and the second flying capacitor 120 are different. Therefore, as shown by the curve C103, the output terminal OUT will form three smaller surges RP10 in one cycle CY2. The reduced surges RP10 can make the ripple of the analog voltage (AVDD) inconspicuous.
透過上述實施例,充放電幫浦電路100可以透過第一飛行電容110及第二飛行電容120交錯地進行充放電動作,使得整體充電的間隔縮短,而能夠減少負類比電壓的漣波(ripple),進而避免產生干擾(crosstalk)現象,以維持良好畫面品質。 Through the above embodiment, the charge and discharge pump circuit 100 can alternately charge and discharge through the first flying capacitor 110 and the second flying capacitor 120, so that the overall charging interval is shortened, and the ripple of the negative analog voltage can be reduced. , Thereby avoiding crosstalk, so as to maintain good picture quality.
請參照第11圖,其繪示根據本發明另一實施例之一第一時序控制訊號ts31及一第二時序控制訊號ts32之示意圖。在此實施例中,第一時序控制訊號ts31之一第一充電期間T31小於一第一放電期間T32,第二時序控制訊號ts32之一第二充電期間T33小於一第二放電期間T34。 Please refer to FIG. 11, which illustrates a schematic diagram of a first timing control signal ts31 and a second timing control signal ts32 according to another embodiment of the present invention. In this embodiment, a first charging period T31 of one of the first timing control signals ts31 is shorter than a first discharging period T32, and a second charging period T33 of one of the second timing control signals ts32 is shorter than a second discharging period T34.
如第11圖所示,第一充電期間T31與第一放電期間T32之比率為2/3,第二充電期間T33與第二放電期間T34之比率為2/3。並且,第一放電期間T32涵蓋第二充電期間T33,第二放電期間T34涵蓋第一充電期間T31。此外,第一充電期間T31與第二充電期間T33等長,第一放電期間T32與第二放電期間T34等長。 As shown in FIG. 11, the ratio of the first charging period T31 to the first discharging period T32 is 2/3, and the ratio of the second charging period T33 to the second discharging period T34 is 2/3. The first discharge period T32 covers a second charging period T33, and the second discharge period T34 covers a first charging period T31. The first charging period T31 is the same length as the second charging period T33, and the first discharging period T32 is the same length as the second discharging period T34.
上述實施例之充放電幫浦電路100係以兩個飛行電容(第一飛行電容110及第二飛行電容120)為例做說明。然而,飛行電容之數量並不局限於兩個,飛行電容之數量亦可增加為三個以上。請參照第12圖,其繪示根據本發明另一實施例之充放電幫浦電路400之示意圖。在本實施例中,充放電幫浦電路400更包括一第三飛行電容430、一第三控制器453、一第五開關465及一第六開關466。第三飛行電容430與第一飛行電容110及第二飛行電容120並聯。時序控制器150係以第三時序控制訊號ts43經由第三控制器453控制第三飛行電容430。 The charge and discharge pump circuit 100 of the above embodiment is described by taking two flying capacitors (a first flying capacitor 110 and a second flying capacitor 120) as an example. However, the number of flying capacitors is not limited to two, and the number of flying capacitors can also be increased to three or more. Please refer to FIG. 12, which illustrates a schematic diagram of a charge-discharge pump circuit 400 according to another embodiment of the present invention. In this embodiment, the charge and discharge pump circuit 400 further includes a third flying capacitor 430, a third controller 453, a fifth switch 465 and a sixth switch 466. The third flying capacitor 430 is connected in parallel with the first flying capacitor 110 and the second flying capacitor 120. The timing controller 150 controls the third flying capacitor 430 through the third controller 453 with a third timing control signal ts43.
在本實施例中,第三時序控制訊號ts43不同於第一時序控制訊號ts41且不同於第二時序控制訊號ts42。請參照第 13圖,其繪示根據本發明一實施例之第一時序控制訊號ts41、第二時序控制訊號ts42及第三時序控制訊號ts43之示意圖。如第13圖所示,第一時序控制訊號ts41之一第一充電期間T41大於一第一放電期間T42,第二時序控制訊號ts42之一第二充電期間T43大於一第二放電期間T44,第三時序控制訊號ts43之一第三充電期間T45大於一第三放電期間T46。第一充電期間T41與第一放電期間T42之比率為2,第二充電期間T43與第二放電期間T44之比率為2,第三充電期間T45與第三放電期間T46之比率為2。 In this embodiment, the third timing control signal ts43 is different from the first timing control signal ts41 and different from the second timing control signal ts42. Please refer to 13 is a schematic diagram illustrating a first timing control signal ts41, a second timing control signal ts42, and a third timing control signal ts43 according to an embodiment of the present invention. As shown in FIG. 13, one of the first timing control signals ts41 has a first charging period T41 greater than a first discharging period T42, and one of the second timing control signals ts42 has a second charging period T43 greater than a second discharging period T44. A third charging period T45 of one of the third timing control signals ts43 is greater than a third discharging period T46. The ratio of the first charging period T41 to the first discharging period T42 is 2, the ratio of the second charging period T43 to the second discharging period T44 is 2, and the ratio of the third charging period T45 to the third discharging period T46 is 2.
此外,第一充電期間T41涵蓋第二放電期間T44及第三放電期間T46,第二充電期間T43涵蓋第一放電期間T42及第三放電期間T46,第三充電期間T45涵蓋第一放電期間T42及第二放電期間T44。並且第一充電期間T41、第二充電期間T43及第三充電期間T45等長,第一放電期間T42、第二放電期間T44及第三充電期間T46等長。 In addition, the first charging period T41 covers the second discharging period T44 and the third discharging period T46, the second charging period T43 covers the first discharging period T42 and the third discharging period T46, and the third charging period T45 covers the first discharging period T42 and The second discharge period T44. The first charging period T41, the second charging period T43, and the third charging period T45 are equal in length, and the first discharging period T42, the second discharging period T44, and the third charging period T46 are equal in length.
請參考第14圖,其繪示同時透過第一時序控制訊號ts41、第二時序控制訊號ts42及第三時序控制訊號ts43進行充放電操作之第一飛行電容110、第二飛行電容120、第三飛行電容430與輸出端OUT之充放電曲線。曲線C141為第一飛行電容110之充放電曲線,曲線C142為第二飛行電容120之充放電曲線,曲線C143為第三飛行電容430之充放電曲線,曲線C144為輸出端OUT之充放電曲線。如曲線C141所示,第一飛行電容110在一個週期CY4進行一次充電動作。如曲線C142所示,第二飛行電容120 在同一周期CY4也進行一次充電動作。如曲線C143所示,第三飛行電容430在同一周期CY4也進行一次充電動作。因此,如曲線C144所示,輸出端OUT在一個周期CY4內會形成三個較小的突波RP14,縮小的突波RP14,可以使類比電壓(AVDD)的漣波變得不明顯。 Please refer to FIG. 14, which shows the first flying capacitor 110, the second flying capacitor 120, the first flying capacitor 110, and the charging and discharging operation through the first timing control signal ts41, the second timing control signal ts42, and the third timing control signal ts43 at the same time. Charge and discharge curves of the three flying capacitors 430 and the output terminal OUT. Curve C141 is the charge and discharge curve of the first flying capacitor 110, curve C142 is the charge and discharge curve of the second flying capacitor 120, curve C143 is the charge and discharge curve of the third flying capacitor 430, and curve C144 is the charge and discharge curve of the output OUT. As shown by the curve C141, the first flying capacitor 110 performs a charging operation in one cycle CY4. As shown by curve C142, the second flying capacitor 120 CY4 also performs a charging operation in the same cycle. As shown by the curve C143, the third flying capacitor 430 also performs a charging operation in the same cycle CY4. Therefore, as shown by the curve C144, the output terminal OUT will form three smaller surges RP14 within a period CY4, and the reduced surges RP14 may make the ripple of the analog voltage (AVDD) inconspicuous.
透過上述實施例,充放電幫浦電路400可以透過第一飛行電容110、第二飛行電容120及第三飛行電容430輪流地進行充放電動作,使得整體充電的間隔縮短,而能夠減少負類比電壓的漣波(ripple),進而避免產生干擾(crosstalk)現象,以維持良好畫面品質。 Through the above embodiment, the charging and discharging pump circuit 400 can perform the charging and discharging operations in turn through the first flying capacitor 110, the second flying capacitor 120, and the third flying capacitor 430, so that the overall charging interval is shortened, and the negative analog voltage can be reduced Ripple, thereby avoiding crosstalk, so as to maintain good picture quality.
綜上所述,雖然本發明已以實施例揭露如上,然其並非用以限定本發明。本發明所屬技術領域中具有通常知識者,在不脫離本發明之精神和範圍內,當可作各種之更動與潤飾。因此,本發明之保護範圍當視後附之申請專利範圍所界定者為準。 In summary, although the present invention has been disclosed as above with the embodiments, it is not intended to limit the present invention. Those with ordinary knowledge in the technical field to which the present invention pertains can make various changes and modifications without departing from the spirit and scope of the present invention. Therefore, the protection scope of the present invention shall be determined by the scope of the attached patent application.
Claims (33)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW106126147A TWI646759B (en) | 2017-08-02 | 2017-08-02 | Charge and discharge pump circuit and control method thereof |
| CN201710875616.7A CN107527585B (en) | 2017-08-02 | 2017-09-25 | Charge/discharge pump circuit and control method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW106126147A TWI646759B (en) | 2017-08-02 | 2017-08-02 | Charge and discharge pump circuit and control method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| TWI646759B true TWI646759B (en) | 2019-01-01 |
| TW201911717A TW201911717A (en) | 2019-03-16 |
Family
ID=60737178
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW106126147A TWI646759B (en) | 2017-08-02 | 2017-08-02 | Charge and discharge pump circuit and control method thereof |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN107527585B (en) |
| TW (1) | TWI646759B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090039947A1 (en) * | 2007-08-08 | 2009-02-12 | Advanced Analogic Technologies, Inc. | Time-Multiplexed-Capacitor DC/DC Converter with Multiple Outputs |
| CN101969265A (en) * | 2009-07-28 | 2011-02-09 | 联咏科技股份有限公司 | Charge pump circuit |
| TW201328155A (en) * | 2011-12-23 | 2013-07-01 | Realtek Semiconductor Corp | Charge pump circuit and method thereof |
| TW201338372A (en) * | 2012-03-05 | 2013-09-16 | Novatek Microelectronics Corp | Charge pump device |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2455524B (en) * | 2007-12-11 | 2010-04-07 | Wolfson Microelectronics Plc | Charge pump circuit and methods of operation thereof and portable audio apparatus including charge pump circuits |
-
2017
- 2017-08-02 TW TW106126147A patent/TWI646759B/en active
- 2017-09-25 CN CN201710875616.7A patent/CN107527585B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090039947A1 (en) * | 2007-08-08 | 2009-02-12 | Advanced Analogic Technologies, Inc. | Time-Multiplexed-Capacitor DC/DC Converter with Multiple Outputs |
| CN101969265A (en) * | 2009-07-28 | 2011-02-09 | 联咏科技股份有限公司 | Charge pump circuit |
| TW201328155A (en) * | 2011-12-23 | 2013-07-01 | Realtek Semiconductor Corp | Charge pump circuit and method thereof |
| TW201338372A (en) * | 2012-03-05 | 2013-09-16 | Novatek Microelectronics Corp | Charge pump device |
Also Published As
| Publication number | Publication date |
|---|---|
| TW201911717A (en) | 2019-03-16 |
| CN107527585B (en) | 2020-06-19 |
| CN107527585A (en) | 2017-12-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8791748B2 (en) | Charge pump circuit and operation control method thereof | |
| KR100516083B1 (en) | Dc-dc converter | |
| US20070159233A1 (en) | Charge pump power supply circuit | |
| US9768682B2 (en) | Switched capacitors with inverted break-before-make without external filtering load capacitor | |
| CN112821757B (en) | Power converter | |
| US20190058403A1 (en) | Comparator circuit, power supply control ic, and switching power supply device | |
| CN108199573B (en) | Soft start circuit and method thereof | |
| US11588391B1 (en) | Power conversion structure, system, method, electronic device including power conversion structure, and chip unit | |
| US20150357916A1 (en) | Buck-boost converter and operating method | |
| US10468979B2 (en) | Electronic device with a charge recycling mechanism | |
| CN108365747B (en) | Switched capacitor DC-to-DC converter circuit and method of producing the same | |
| US20070236972A1 (en) | Semiconductor integrated circuit device, charge pump circuit, and electric appliance | |
| TWI646759B (en) | Charge and discharge pump circuit and control method thereof | |
| JP5767660B2 (en) | DC-DC converter | |
| CN107395012A (en) | A kind of charge pump circuit and its control method | |
| KR102858074B1 (en) | Voltage conversion circuit, voltage converter, and chip | |
| JP2010283952A (en) | Charge pump circuit | |
| CN102594133B (en) | Boosting method and boosting circuit | |
| US9350235B2 (en) | Switched capacitor voltage converting device and switched capacitor voltage converting method | |
| CN118525441A (en) | Switching power supply and control method thereof, power supply system and electronic equipment | |
| US20250096682A1 (en) | On-time Generator Circuit and Switching Converter | |
| US9490073B2 (en) | Electronic device | |
| US20090303755A1 (en) | Power converter apparatus | |
| US7053632B1 (en) | Circuit and method for predicting dead time | |
| KR100747212B1 (en) | Switch Capacitor Converter and Control Method |